NATOPS Chapter 2 Engine HSM-50 Flashcards

1
Q

Indications of Impending High Speed Shaft Failure

A

high-intensity, medium to high freq vibs (may vary with movement of PCL)
howl

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2
Q

With high speed shaft failure, Np is __ than Nr by more than __; torque will be ___

A

greater, 3%

below 10%

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3
Q

Altitude required for dual engine restart

A

5000 ft AGL

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4
Q

Indications of Malfunctioning Engine Anti-Ice/Start Bleed

A
  1. Appearance or disappearance of ENG ANTI-ICE ON advisory when outside of range specified (80.5% to 96.5% Ng)
  2. No ENG ANTI-ICE ON when ENG ANTI-ICE switch on
  3. No rise in TGT when ENG ANTI-ICE ON
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5
Q

MH-60R Engine

A

T700-GE-401C front drive turboshaft

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6
Q

5 sections of engine

A

inlet, compressor, combustor, turbine, exhaust

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7
Q

Airflow/mechanical energy through engine

A

inlet cowling –> swirl vanes –> collection scroll –> scroll vanes (in collection scroll) –> overboard through blower assembly or to deswirl vanes –> compressor –> combustor –> Ng turbine –> Np turbine –> high speed shaft –> input module –> xsmn

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8
Q

inlet anti-ice valve uses ___ and works by __

A

5th stage bleed air; heating exposed inlet surface with the hot air

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9
Q

swirl vanes are hollow to permit passage of

A

5th stage bleed air via engine anti-ice valve for anti-icing purposes

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10
Q

purpose of IPS

A

prevent foreign particles from entering compressor

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11
Q

compressor

A

five stage axial and single stage centrifugal rotor/stator assembly

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12
Q

combustion section

A

flow through, annular combustion chamber, two igniters, 12 fuel injectors

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13
Q

Fuel injectors receive fuel from __ and supply __

A

ODV; atomized fuel for combustion

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14
Q

Ng turbine drives

A

compressor and AGB

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15
Q

Ng turbine is

A

two stage, air cooled, high performance axial design

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16
Q

Np turbine

A

2 stages that turn power turbine drive shaft

17
Q

power turbine drive shaft

A

coaxial, turning inside Ng turbine drive shaft

drives high speed shaft which is connected to input module

18
Q

Engine Airflow usage

A

30% for combustion, 70% for:

  1. T2
  2. P3
  3. Combustor and turbine cooling
  4. Engine oil seal pressurization
19
Q

T2

A

compressor inlet temp air

20
Q

P3

A

compressor discharge pressure air

21
Q

AGB mounts to __; front and rear faces provide drive pads for

A

rear of main frame at 12 oclock position, above scroll case

rear face: engine starter, HMU, IPS blower, ODV
front face: alternator and engine driven fuel boost pump

22
Q

AGB is driven by

A

a rotor via a radial drive shaft from Ng turbine drive shaft

23
Q

Describe airflow through the engine

A

inlet cowling - swirl vanes - collection scroll - [IPS - overboard through blower assembly] - deswirl vanes - compressor - Ng turbine - Np turbine